Technical Field
[0001] The present invention relates to a sputtering target and a method for manufacturing
the same, and more particularly, to an indium target and a method for manufacturing
the same.
Background Art
[0002] Indium has been used as a sputtering target for forming a light absorbing layer for
Cu-In-Ga-Se-based (CIGS-based) thin film solar cells.
[0003] Indium targets are conventionally manufactured mainly according to a melting and
casting method.
Japanese Patent Application Publication No.
63-44820 (Patent Literature 1) describes a method of forming a thin film of indium on a backing
plate, subsequently pouring indium on the thin film to cast indium, and thereby forming
an indium target integrally with the backing plate.
Furthermore, Japanese Patent Application Laid-Open (JP-A) No.
2010-24474 (Patent Literature 2) describes a method of manufacturing an indium target including
the steps of feeding a predetermined amount of an indium raw material into a heated
mold for melting, removing indium oxide that floats on the surface, cooling the molten
indium to obtain an ingot, and grinding the surface of the ingot to obtain an indium
target, wherein the predetermined amount of the indium raw material is not fed to
the mold all at once but is fed in several divided portions, indium oxide formed on
the molten metal surface is removed each time, and then the ingot obtained by cooling
the molten metal is surface ground.
Citation List
Patent Literature
Summary of Invention
Technical Problem
[0005] However, in the case of manufacturing an indium target by such a melting and casting
method, if the cooling rate is high, there has been a problem that pores are produced
in the interior of the target, and therefore, arcing eventually occurs during sputtering.
On the other hand, if the cooling rate is decreased, there has been a problem that
the grain size increases, and the deposition rate decreases.
[0006] Thus, an object of the present invention is to provide an indium target which is
capable of achieving a high deposition rate while suppressing the occurrence of arcing,
and a method for manufacturing the indium target.
Solution to Problem
[0007] The inventors of the present invention conducted a thorough investigation in order
to solve the problems described above, and found that in a solidification process
at the time of melting and casting of an indium ingot, when ultrasonic vibration is
applied to molten indium liquid which is at least in a state immediately before solidification,
the grain size of the indium ingot thus obtainable can be significantly reduced. It
is not intended to have the present invention limited by theory, but it is speculated
that this is because the ultrasonic vibration causes a large number of crystal nuclei
to be formed at a high density, so that the gaps between grains are reduced, and coarsening
of grain is suppressed.
As a result, even if the cooling rate at the time of melting and casting is decreased
in order to prevent the generation of pores in the target, which is causative of arcing,
since coarsening of grains is suppressed, a target having a high deposition rate is
obtained.
[0008] According to an aspect of the present invention that has been accomplished based
on the findings described above, there is provided An indium target wherein:
an overall average grain size is 10 mm or less;
for the grains observed from a cross-section parallel to a thickness direction, a
ratio of an average grain size in a direction parallel to the thickness direction
with respect to an average grain size in a direction perpendicular to the thickness
direction is 0.7 to 1.1; and
pores with a pore size of 50 µm or greater exists at a density of 1 pore/cm3 or less.
[0009] According to an embodiment of the present invention, the indium target has a maximum
grain size of 20 mm or less.
[0010] According to another aspect of the present invention, there is provided a method
for manufacturing an indium target, the method including a step of melting and casting
an indium raw material, while ultrasonic vibration is applied at least at the time
of solidification of the indium raw material.
[0011] According to an embodiment of the present invention, the method for manufacturing
an indium target includes cooling at the time of melting and casting at a cooling
rate of 3°C/min to 70°C/min.
Advantageous Effects of Invention
[0012] According to the present invention, an indium target is obtained, which is capable
of maintaining a high deposition rate while suppressing the occurrence of arcing.
Furthermore, in the present invention, since indium has no added impurities such as
a grain refining agent, an effect of facilitating the recycling of targets is also
obtained.
Brief Description of Drawing
[0013]
FIG. 1 is a schematic diagram illustrating the direction perpendicular to the thickness
direction, x, and the direction parallel to the thickness direction, y, employed when
the cross-sectional aspect ratio is measured.
Description of Embodiment
[0014] The present invention is characterized in that in the solidification process at the
time of melting and casting of an indium ingot, ultrasonic vibration is applied to
molten indium liquid in a state immediately before solidification, and thereby, coarsening
of the grain size is suppressed. According to the present invention, the overall average
grain size of the indium target can be controlled to 10 mm or less. In general, when
an indium ingot is produced by a melting and casting method, if it is intended to
avoid the generation of pores in the indium ingot, it is necessary to perform cooling
at a cooling rate that is slow to a certain extent. In this case, the average grain
size increases to about 40 mm or greater. With such a large grain size, the deposition
rate of the sputtering process is reduced. However, in the present invention, the
growth of grains can be suppressed even at such a slow cooling rate, by applying ultrasonic
vibration at the time of solidification. Furthermore, the application of ultrasonic
vibration also has an effect of suppressing the amount of pores.
[0015] When the overall average grain size decreases, the deposition rate increases correspondingly.
However, since there are limitations on the reduction of grains, the overall average
grain size is preferably 1 mm to 6 mm, and more preferably 1 mm to 3 mm.
[0016] Furthermore, according to an embodiment of the present invention, since the indium
target can be manufactured without carrying out cold rolling after the process of
melting and casting, the indium target is also characterized in that the ratio of
the average grain size in a direction parallel to the thickness direction with respect
to the average grain size in a direction perpendicular to the thickness direction,
in the grains observed from a cross-section that is parallel to the thickness direction
(hereinafter, also referred to as "cross-sectional aspect ratio") is close to 1, that
is, the grains are not flat. Specifically, the cross-sectional aspect ratio is 0.7
to 1.1, and typically 0.8 to 1.0.
[0017] According to the present invention, the overall average grain size of the indium
target is measured by the following method. The surface of a target is lightly etched
with a weak acid. Alternatively, carbon powder is applied to the surface to make the
grain boundaries easily visible, subsequently an arbitrary area measuring 25 mm ×
50 mm on the target surface is defined as a region to be measured, and the number
of grains (N) in the region is counted by visual inspection. A grain which exists
over the boundary of the region is handled as 0.5 grains. The average area of the
grains (s) is calculated by dividing the area of the region to be measured (S = 1250
mm
2) by the number of grains (N). Assuming that the grains are spherical, the average
grain size (A) is calculated by the following formula:

[0018] According to the present invention, the cross-sectional aspect ratio is measured
by the following method. With reference to FIG. 1, a target is cut in an arbitrary
thickness direction such that the cut surface passes the central axis 11 of the target
10. Subsequently, the exposed cut surface 12 is lightly etched with a weak acid. Alternatively,
carbon powder is applied on the cut surface 12 to make the grain boundaries easily
visible, and then any twenty grains are designated as objects of measurement. The
average grain size (a) in a direction x perpendicular to the thickness direction,
and the average grain size (b) in a direction y parallel to the thickness direction
are calculated by visual inspection, and thereby the cross-sectional aspect ratio
(b/a) is determined.
The average grain size in a direction perpendicular to the thickness direction is
the average value for the grains as the objects of measurement, provided that the
longest line segment perpendicular to the thickness direction that can be circumscribed
by each grain is designated as the grain size in the direction perpendicular to the
thickness for each grain.
The average grain size in a direction parallel to the thickness direction is the average
value for the grains as the objects of measurement, provided that the longest line
segment parallel to the thickness direction that can be circumscribed by each grain
is designated as the grain size in the direction parallel to the thickness for each
grain.
[0019] According to a preferred embodiment of the present invention, the indium target has
a maximum grain size of 20 mm or less. By controlling the maximum grain size to 20
mm or less in addition to the overall average grain size of the target, the fluctuation
in the grain size distribution is decreased. Thereby, the change in the deposition
rate of sputtering is reduced, and also, in particular, regions with slow deposition
rates are eliminated. The maximum grain size is preferably 15 mm or less, and more
preferably 10 mm or less, for example, 5 mm to 10 mm.
[0020] According to the present invention, the maximum grain size of the indium target is
measured by the following method. Based on the area of the largest grain (smax) among
the grains in the area to be measured at the time of measuring the overall average
grain size of the indium target as described above, the maximum grain size (B) is
calculated by the following formula assuming that the grain is spherical:

[0021] According to a preferred embodiment of the present invention, the indium target has
pores having a pore size of 50 µm or greater at a density of 1 pore/cm
3 or less. Pores that are present in the interior of the target, particularly, large
pores having a pore size of 50 µm or greater, cause the occurrence of arcing during
sputtering, and therefore, it is preferable to reduce the pores as much as possible.
According to the present invention, since there is provided an effect of suppressing
the coarsening of grains by ultrasonic vibration, cooling can be carried out at a
slow cooling rate, which suppresses the generation of pores at the time of melting
and casting of the ingot. Therefore, grain refinement and prevention of the generation
of pores can be compatibly achieved. The density of pores having a pore size of 50
µm or greater is preferably 0.5 pores/cm
3 or less, and more preferably 0.3 pores/cm
3 or less, for example, 0 to 0.3 pores/cm
3.
[0022] According to the present invention, the number density of pores having a pore size
of 50 µm or greater is measured with an electron scanning ultrasonic probe. A target
is placed in the probe water bath of the apparatus, and measurement is made at a frequency
range of 1.5 = 20 MHz, a pulse repetition frequency of 5 kHz, and a scan speed of
60 mm/min. Pores having a pore size of 50 µm or greater are counted from the image
thus obtainable, and thereby, the number density of the pores is determined from the
volume of the target to be measured. Here, the pore size is defined as the diameter
of the smallest circle that circumscribes a pore in the image.
[0023] Next, a suitable example of the method for manufacturing an indium target according
to the present invention will be described in order. First, the raw material indium
is melted and poured into a mold. The raw material indium to be used desirably has
high purity, for the reason that if impurities are included, the conversion efficiency
of a solar cell manufactured from the raw material is decreased. For example, a raw
material having a purity of 99.99% by mass or higher can be used. Subsequently, the
raw material indium is cooled to room temperature, and thus an indium ingot is formed.
From the viewpoint of accelerating the production of a large number of crystal nuclei
at the time of initiation of crystallization, it is necessary to carry out the application
of ultrasonic waves at least at the time of solidification of the indium raw material.
[0024] Specifically, it is preferable that the temperature be decreased slowly from the
melting temperature of indium, and the application of ultrasonic waves be initiated
at least when the temperature has decreased to a value immediately above the melting
point of indium of 156 °C (for example, 157°C to 160°C). Ultrasonic vibration may
also be applied at a time point where the temperature is still higher than this, that
is, while indium is in a molten state, but it is somehow meaningless. It is important
to apply ultrasonic vibration immediately before solidification. Furthermore, the
application may be continued until the solidification of indium is completed, but
this is also unnecessary, and the application of ultrasonic vibration may be stopped
at a time point where, for example, the temperature of indium has decreased to about
159°C, and typically to about 157°C.
[0025] There are no particular limitations on the method of applying ultrasonic vibration,
and any known method can be employed. However, for example, a method of applying ultrasonic
vibration to a molten indium liquid immediately before solidification by using an
apparatus based on the principle that an electrostriction type vibrator vibrates at
a high frequency, amplifying the vibration of the vibrator with an amplifier, subsequently
transferring the vibration to an ultrasonic vibration horn, and inserting this ultrasonic
vibration horn directly into molten indium, is preferred because ultrasonic vibration
can be directly applied to the interior of indium.
[0026] Cooling at the time of solidification may be achieved by natural cooling by air
(about 10°C/min), but when the cooling rate is decreased, for example, to a rate of
9°C/min or less, and preferably to a rate of 8°C/min or less, an effect of further
suppressing the generation of pores in the ingot may be obtained. However, if the
cooling rate is too slow, the effect of suppressing the coarsening of crystals by
ultrasonic vibration may not be sufficiently obtained in this case. Therefore, it
is preferable to set the cooling rate to 3°C/min or higher, and it is more preferable
to set the cooling rate to 5°C/min or higher. On the other hand, in the case of emphasizing
the prevention of the growth of grain size, the cooling rate can also be increased.
For example, the cooling rate can be set to 20°C/min or higher, and preferably to
50°C/min. However, if the cooling rate is too high, the amount of pores is likely
to increase in this case, and therefore, it is preferable to perform cooling at a
rate of 70°C/min even at the maximum. Particularly, since ultrasonic vibration is
applied in the present invention, the rate of increase of the amount of pores is smaller
than the rate of increase of the cooling rate. Accordingly, when the cooling rate
is set to a slightly high value, a high deposition rate can be achieved, and a high
level of suppression of arcing can be also achieved.
The adjustment of the cooling rate can be carried out, in the case of decreasing the
cooling rate, by heating the mold and keeping it heated with a heater or the like;
and in contrast, in the case of increasing the cooling rate, by a water cooling method
or the like involving supplying cooling water to the periphery of the mold. The cooling
rate here is calculated by the formula: (melting temperature of indium - 25°C) / (time
taken until the temperature of indium decreases from the melting temperature to 25°C
after the initiation of cooling). After the process of melting and casting, the indium
ingot is subjected to a shape processing or surface polishing as necessary, and thereby
an indium target is obtained.
[0027] The thickness of the target is not particularly limited, and may be appropriately
set in accordance with the sputtering apparatus to be used, the time of use in film
formation, or the like. However, the thickness is usually about 3 mm to 20 mm, and
typically about 5 mm to 10 mm.
[0028] An indium target thus obtained can be suitably used as a sputtering target for the
manufacture of light absorbing layers for CIGS-based thin film solar cells.
Examples
[0029] Hereinafter, Examples of the present invention will be disclosed together with Comparative
Examples, but these Examples are provided only for the purpose of making the present
invention and advantages thereof more understandable, and are not intended to limit
the invention by any means.
[0030] An indium raw material (purity: 5 N) was melted at 170°C, and this molten body was
poured into a cylindrical mold having a diameter of 250 mm and a height of 7 mm. The
indium raw material was cooled to room temperature (25°C) at the cooling rate indicated
in Table 1, and thus an indium ingot was manufactured. At this time, in the Invention
Examples, application of ultrasonic vibration was initiated at 160°C, which was immediately
above the solidification temperature of indium. Ultrasonic vibration was applied to
the molten indium liquid immediately before solidification by using an apparatus based
on the principle that an electrostriction type vibrator vibrates at a high frequency,
amplifying the vibration of the vibrator with an amplifier, subsequently transferring
the vibration to an ultrasonic vibration horn, and inserting this ultrasonic vibration
horn directly into molten indium. While the temperature of the molten metal to which
vibration was being applied was measured with a thermocouple for temperature measurement,
the ultrasonic vibration horn was pulled out when the temperature decreased to 156°C,
and thereby the application of ultrasonic vibration was stopped. Subsequently, the
ingot was processed into a disc shape having a diameter of 204 mm and a thickness
of 6 mm, and used as a sputtering target for each of Invention Examples and Comparative
Examples.
[0031] For the indium targets thus obtained, the property values of the following items
A to D were measured by the methods described earlier.
For the measurement of the items A to C, a commercially available carbon powder was
used for surface polishing, and the measurement was made by visual observation.
For the measurement of the item D, an electron scanning ultrasonic probe system, PA-101,
manufactured by Krautkramer Japan Co., Ltd. was used.
The results are presented in Table 1.
- A: Overall average grain size
- B: Maximum grain size
- C: Cross-sectional aspect ratio of a grain
- D: Number density of pores having a pore size of 50 µm or greater
[0032] Furthermore, each of these indium targets of Invention Examples and Comparative Examples
was used to deposit a film for 5 min by using #1737 glass manufactured by Corning,
Inc. as a substrate without heating the substrate, with an SPF-313H apparatus manufactured
by Canon Anelva Corp., while adjusting the ultimate vacuum pressure in the chamber
before the initiation of sputtering to 1 × 10
-4 Pa, flowing argon gas at 5 sccm, and adjusting the pressure at the time of sputtering
to 0.5 Pa and the sputtering power to 650 W. The results are presented in Table 2.
Table 2 describes the deposition rate and the arcing count during sputtering.
The deposition rate was calculated from the deposition time and the results of measuring
the film thickness with a step gauge, and the arcing counts was measured by a method
of visual inspection.
[0033]
[Table 1]
No. |
Ultrasonic vibration |
Cooling rate (°C/min) |
A (mm) |
B (mm) |
C |
D (pores/cm3) |
Comparative Example 1 |
Absent |
10 (natural cooling) |
20 |
32 |
0.83 |
0.7 |
Invention Example 1 |
Present |
10 (natural cooling) |
5 |
13 |
0.85 |
0.3 |
Comparative Example 2 |
Absent |
100 (high rate cooling) |
2 |
7 |
0.93 |
2.5 |
Invention Example 2 |
Present |
5 (low rate cooling) |
8 |
18 |
0.75 |
0 |
Comparative Example 3 |
Present |
1 (ultralow rate cooling) |
15 |
26 |
0.69 |
0.1 |
Invention Example 3 |
Present |
70 (high rate cooling) |
2 |
8 |
0.88 |
0.9 |
[0034]
[Table 21
No. |
Deposition rate (nm/min) |
Arcing counts |
Comparative Example 1 |
350 |
0 |
Invention Example 1 |
401 |
0 |
Comparative Example 2 |
410 |
20 |
Invention Example 2 |
396 |
0 |
Comparative Example 3 |
369 |
0 |
Invention Example 3 |
405 |
0 |
[0035] The following is understood from Table 1 and Table 2. Comparative Example 1 is an
example of natural cooling without ultrasonic vibration, and the average grain size
became excessively large. As a result, the deposition-rate became low.
In Invention Example 1, natural cooling was carried out in the same manner as in Comparative
Example 1, but as ultrasonic vibration was applied, the average grain size decreased,
and the deposition rate was enhanced.
In Comparative Example 2, the average grain size was made small by high rate cooling,
but since ultrasonic vibration was not applied, the amount of pores increased. As
a result, the arcing counts increased.
In Invention Example 2, since the cooling rate was made slightly lower than that of
Invention Example 1, the average grain size was slightly larger. However, as ultrasonic
vibration was applied, the average grain size was smaller than that of Comparative
Example 1.
Comparative Example 3 is an example in which, although ultrasonic vibration was applied,
since the cooling rate was made too slow, the average grain size became excessively
large.
Invention Example 3 is an example in which the deposition rate was increased by increasing
the cooling rate. Although the cooling rate was quite high, an increase in the amount
of pores was suppressed, and no arcing was observed.
[0036]
Reference Signs List
10 |
Target |
11 |
Central axis |
12 |
Cut surface |
x |
Perpendicular direction |
y |
Parallel direction |